☆ 4.7 Article

Robust control of gust-induced vibration of highly flexible aircraft

AEROSPACE SCIENCE AND TECHNOLOGY (2023)

相关参考文献

注意：仅列出部分参考文献，下载原文获取全部文献信息。

Article Automation & Control Systems

Computation of parameter dependent robust invariant sets for LPV models with guaranteed performance?

Ankit Gupta et al.

Summary: This paper proposes an iterative algorithm to compute the Robust Control Invariant (RCI) set and the corresponding control law for Linear Parameter-Varying (LPV) systems. The algorithm considers the dependence of RCI set description and control law on scheduling parameters. By replacing parameter-dependent conditions for set invariance with Linear Matrix Inequalities (LMIs) using Polya's relaxation, a Semidefinite Programming (SDP) problem is formulated to maximize the volume of the RCI set. The presented algorithm outperforms commonly used robust approaches in handling large parameter variations.

AUTOMATICA (2023)

添加到收藏夹

Article Engineering, Aerospace

Nonlinear Model Predictive Control of J2-perturbed impulsive transfer trajectories in long-range rendezvous missions

Sanaz Samsam et al.

Summary: This paper presents a Nonlinear Model Predictive Control (NMPC) strategy for robust tracking of multi-impulse smooth transfer trajectories in J2-perturbed orbital environments. It proposes a variable prediction horizon NMPC with velocity increments as control signals and uses equinoctial orbital elements to avoid singularities. The NMPC calculates the optimal correction control vector to minimize deviation and control effort, and an evolutionary optimization algorithm is implemented to handle impulsive control inputs.

AEROSPACE SCIENCE AND TECHNOLOGY (2023)

添加到收藏夹

Article Engineering, Aerospace

Linear parameter-varying-based transition flight control design for a tilt-rotor aircraft

Shen Qu et al.

Summary: This paper presents the development of novel transition flight controllers for urban air mobility aircrafts. The controllers utilize fixed-wing and six electric rotor assemblies to achieve stable altitude control by adjusting rotor angles and aerodynamic lift. A series of linear models are obtained by linearizing the nonlinear aircraft model, and a novel transition flight control architecture is developed using these models. The simulation results demonstrate the effectiveness and robustness of the controllers.

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING (2022)

添加到收藏夹

Article Engineering, Aerospace

A cooperative particle swarm optimization approach for tuning an MPC-based quadrotor trajectory tracking scheme

Aristotelis Kapnopoulos et al.

Summary: This paper presents a novel method for tuning a quadrotor trajectory-tracking model predictive control framework using cooperative particle swarm optimization. The method decomposes the overall control strategy into two schemes, utilizing MPC for position control and PID controllers for attitude regulation. It introduces a cooperative PSO framework to optimize the control parameters by exchanging information between two swarms. Simulation results and comparisons demonstrate the effectiveness and robustness of the proposed scheme in optimizing the quadrotor's trajectory tracking performance.

AEROSPACE SCIENCE AND TECHNOLOGY (2022)

添加到收藏夹

Article Engineering, Aerospace

Turbo-fan engine acceleration control schedule optimization based on DNN-LPV model

Ziyu Gu et al.

Summary: This paper proposes a local receding-horizon optimization method with the structure of model predictive control for optimizing the acceleration control schedule of an aero-engine. It also introduces a novel online data-driven linear parameter varying model based on a special structure deep neural network for establishing the predictive model. The effectiveness of the proposed method is validated through simulation results.

AEROSPACE SCIENCE AND TECHNOLOGY (2022)

添加到收藏夹

Article Engineering, Aerospace

Gust load alleviation for flexible aircraft using discrete-time H∞ preview control

A. Khalil et al.

Summary: This paper proposes a methodology for designing Gust Load Alleviation systems, relying on wind profile and optimal control techniques, and introduces a variant to allow design trade-offs and specify robustness criteria. The method is intended for large aircraft, and simulation results demonstrate the effectiveness of the design methodology in considering wind profile while achieving design flexibility and controller optimality.

AERONAUTICAL JOURNAL (2021)

添加到收藏夹

Article Engineering, Aerospace

Adaptive control for linear parameter-varying systems with application to a VTOL aircraft

Steven Snyder et al.

Summary: This paper presents design and analysis of an adaptive control architecture for LPV systems subject to time-varying parametric uncertainties and external disturbances, with both transient and steady-state performance guarantees. The approach introduces new tools and techniques for stability and performance analysis, potentially yielding less conservative results compared to previous methods.

AEROSPACE SCIENCE AND TECHNOLOGY (2021)

添加到收藏夹

Article Engineering, Aerospace

The balanced mode decomposition algorithm for data-driven LPV low-order models of aeroservoelastic systems

Andrea Iannelli et al.

Summary: This novel approach combines Dynamic Mode Decomposition with balanced realization to achieve reduced-order modeling of high-dimensional systems with time-varying properties in a fully data-driven manner. The goal is to obtain a low-dimensional linear model approximating the system within its operating range, while retaining time-varying features through a collection of state-consistent linear time-invariant reduced-order models. The method replaces orthogonal projection with a balancing oblique projection constructed from data to increase input-output information captured in the lower-dimensional representation.

AEROSPACE SCIENCE AND TECHNOLOGY (2021)

添加到收藏夹

Article Automation & Control Systems

Heterogeneously parameterized tube model predictive control for LPV systems

Jurre Hanema et al.

AUTOMATICA (2020)

添加到收藏夹

Article Engineering, Aerospace

Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

X. Wang et al.

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2019)

添加到收藏夹

Article Engineering, Aerospace

Smooth-switching LPV control for vibration suppression of a flexible airplane wing

Tianyi He et al.

AEROSPACE SCIENCE AND TECHNOLOGY (2019)

添加到收藏夹

Article Engineering, Aerospace

AEROM: NASA's Unsteady Aerodynamic and Aeroelastic Reduced-Order Modeling Software

Walter A. Silva

AEROSPACE (2018)

添加到收藏夹

Article Engineering, Aerospace

LQG based model predictive control for gust load alleviation

Xiang Liu et al.

AEROSPACE SCIENCE AND TECHNOLOGY (2017)

添加到收藏夹

Article Automation & Control Systems

Stabilizing tube-based model predictive control: Terminal set and cost construction for LPV systems

Jurre Hanema et al.

AUTOMATICA (2017)

添加到收藏夹

Article Engineering, Aerospace

LPV modeling of a flexible wing aircraft using modal alignment and adaptive gridding methods

Ali Khudhair Al-Jiboory et al.

AEROSPACE SCIENCE AND TECHNOLOGY (2017)

添加到收藏夹

Article Engineering, Aerospace

Optimum Wing Shape of Highly Flexible Morphing Aircraft for Improved Flight Performance

Weihua Su et al.

JOURNAL OF AIRCRAFT (2016)

添加到收藏夹

Article Energy & Fuels

Real-time wind field reconstruction from LiDAR measurements using a dynamic wind model and state estimation

P. Towers et al.

WIND ENERGY (2016)

添加到收藏夹

Article Engineering, Civil

Problems in geometrically exact modeling of highly flexible beams

P. Frank Pai

THIN-WALLED STRUCTURES (2014)

添加到收藏夹

Article Engineering, Aerospace

Robust Gust Alleviation and Stabilization of Very Flexible Aircraft

Robert G. Cook et al.

AIAA JOURNAL (2013)

添加到收藏夹

Article Engineering, Aerospace

Model-Predictive Gust Load Alleviation Controller for a Highly Flexible Aircraft

Sohrab Haghighat et al.

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2012)

添加到收藏夹

Review Engineering, Aerospace

Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics

Joseba Murua et al.

PROGRESS IN AEROSPACE SCIENCES (2012)

添加到收藏夹

Article Engineering, Aerospace

Dynamic Response of Highly Flexible Flying Wings

Weihua Su et al.

AIAA JOURNAL (2011)

添加到收藏夹

Article Mechanics

Strain-based geometrically nonlinear beam formulation for modeling very flexible aircraft

Weihua Su et al.

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES (2011)

添加到收藏夹

Article Engineering, Aerospace

Structural and Aerodynamic Models in Nonlinear Flight Dynamics of Very Flexible Aircraft

Rafael Palacios et al.

AIAA JOURNAL (2010)

添加到收藏夹

Article Engineering, Aerospace

Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft

Weihua Su et al.

JOURNAL OF AIRCRAFT (2010)

添加到收藏夹

Article Engineering, Aerospace

Adaptive Feedforward Control for Gust Load Alleviation

Jie Zeng et al.

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2010)

添加到收藏夹

Article Engineering, Aerospace

Simultaneous excitation of multiple-input/multiple-output CFD-based unsteady aerodynamic systems

Walter A. Silva

JOURNAL OF AIRCRAFT (2008)

添加到收藏夹

Article Engineering, Aerospace

Nonlinear flight dynamics of very flexible aircraft

Christopher M. Shearer et al.

JOURNAL OF AIRCRAFT (2007)

添加到收藏夹

Article Engineering, Aerospace

Flight dynamics of highly flexible flying wings

Mayuresh J. Patil et al.

JOURNAL OF AIRCRAFT (2006)

添加到收藏夹

Article Engineering, Aerospace

Geometrically exact, intrinsic theory for dynamics of curved and twisted anisotropic beams

DH Hodges

AIAA JOURNAL (2003)

添加到收藏夹

Review Engineering, Aerospace

Aeroelasticity of nonconventional airplane configurations - Past and future

E Livne et al.

JOURNAL OF AIRCRAFT (2003)

添加到收藏夹

Article Engineering, Aerospace

Linear parameter-varying modeling and control of structural dynamics with aerothermoelastic effects

R Lind

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2002)

添加到收藏夹

Article Engineering, Aerospace

Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft

MJ Patil et al.

JOURNAL OF AIRCRAFT (2001)

添加到收藏夹

Article Engineering, Aerospace

Comparing linear parameter-varying gain-scheduled control techniques for active flutter suppression

JM Barker et al.

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2000)

添加到收藏夹

Article Engineering, Aerospace

Robust longitudinal flight control design using linear parameter-varying feedback

MS Spillman

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS (2000)

添加到收藏夹

Article Engineering, Aerospace

Nonlinear aeroelastic analysis of complete aircraft in subsonic flow

MJ Patil et al.

JOURNAL OF AIRCRAFT (2000)

添加到收藏夹

© Peeref 2019-2024. All rights reserved.